[go: up one dir, main page]

BROWN, 1965 - Google Patents

Attitude control system for the direct measurement explorer-A satellite(Attitude control system, using magnetic interaction with geomagnetic field to check spin rate and …

BROWN, 1965

Document ID
15733810542747767618
Author
BROWN R
Publication year

External Links

Continue reading at scholar.google.com (other versions)

Similar Documents

Publication Publication Date Title
BROWN Attitude control system for the direct measurement explorer-A satellite(Attitude control system, using magnetic interaction with geomagnetic field to check spin rate and spin axis orientation of spin-stabilized Explorer A satellite)
COPE Attitude control for sun-pointing scientific satellites(Attitude control for sun-pointing scientific satellites, considering control loop, sun sensor and actuator control torques)
ISRAEL Determination of attitude during flight of v-27 veronique rocket using magnetic aspect sensors
FROEHLICH et al. Some results of the development of the passive magnetic attitude control system for the German research satellite 625 A-1(Acquisition phase of satellite with passive magnetic attitude stabilization, discussing programming difficulities and modified Rayleigh model for German 625 A-1 satellite)
SUNESSON Design of attitude loops for the L. A. S(Guidance sensor loops design for ESRO large astronomical satellite attitude control)
BISMUT et al. Attitude control of a near-earth space probe(Development, design and test operation of attitude control system of space probe with mission duration of 7 minutes)
LINDSAY The combined effect of gravity gradient and aerodynamic torques on the attitude control of the Apollo/S-4 B in a circular orbit about the earth(Aerodynamic and gravity gradient torque effects on attitude control of Apollo/S-4 B configuration in circular earth orbit)
KING Discussion of the nighttime and daytime relationships between magnetic and ionospheric variations
MESCH et al. Investigations on magnetically controlled near earth satellites(Motion equation for satellite with passive and semipassive attitude control using geomagnetic field, considering elliptical and circular orbits and involving differential equations)
KRASOVSKII Thermal noise of measuring instruments and limiting precision of spaceship autonomous control system(Thermal noise in internal measuring instruments affecting limitations on spacecraft open-loop inertial autonomous control system precision)
ERICSON et al. Magnetoaerodynamic drag and flight control(Magnetoaerodynamic drag and flight control available to vehicle entering earth atmosphere calculated, including induced magnetic fields effects and nonscalar conductivity)
BROWN Fluid power control
FORSYTH Design plan for the basic system for vector magnetic field measurements from a javelin rocket nose cone scientific report no. 2, 1 jan.- 30 nov. 1964(Basic system design plan for vector magnetic field measurements from Javelin rocket nose cone, and ground tracking of trajectory and attitude by electromagnetic sensor)
ELVAIN Design considerations for spin axis control of dual-spin spacecraft(Design of spin axis and velocity control system for dual-spin spacecraft)
ABZUG Perturbation analysis of a satellite attitude control system consisting of three inertia-wheels in a closed-loop arrangement
PAUL et al. Gravity-gradient effect utilized to design earth pointing satellite attitude control system, giving a description of the dynamic principles and major components of the system
NAGEL Space navigation instrumentation is discussed, specifically the use of infrared sensors in space vehicles
WHEELER Two-pulse attitude control system for an asymmetric, spinning, earth satellite oriented with its spin axis normal to the plane of its orbit
MERRICK et al. Exploitation of inertial coupling in passive gravity-gradient-stabilized satellites(Exploitation of inertial coupling in passive gravity-gradient-stabilized satellites)
WILD Radio-compass nondirectional aircraft antenna location and its influence on correct flight indication
BROWNLOW Arguments/by nasa/ for a zero-zero weather landin system with active roles for the pilots and space crewmen
GATLIN et al. Gravity gradient attitude control system Patent(Gravity gradient attitude control system with gravity gradiometer and reaction wheels for artificial satellite attitude control)
HARRIS et al. Approaches to the solution of the despin control problem(Sampled data controlled despin system for dual spin spacecraft attitude control)
MELZNER Instrumentation of a Rubis research rocket(Design and instrumentation of Rubis research rocket payload for analysis of geomagnetic and electric fields)
ERICSON et al. Magnetoaerodynamic drag and flight control(Magnetoaerodynamic drag and flight control, considering magnetic field effect carried onboard hypersonic reentry vehicle)